RU2468226C2 - Покрытие для акустической обработки, передняя кромка и воздухозаборник летательного аппарата, содержащие такое покрытие - Google Patents

Покрытие для акустической обработки, передняя кромка и воздухозаборник летательного аппарата, содержащие такое покрытие Download PDF

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Publication number
RU2468226C2
RU2468226C2 RU2009134982/06A RU2009134982A RU2468226C2 RU 2468226 C2 RU2468226 C2 RU 2468226C2 RU 2009134982/06 A RU2009134982/06 A RU 2009134982/06A RU 2009134982 A RU2009134982 A RU 2009134982A RU 2468226 C2 RU2468226 C2 RU 2468226C2
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RU
Russia
Prior art keywords
coating
level
channels
acoustic processing
aircraft
Prior art date
Application number
RU2009134982/06A
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English (en)
Russian (ru)
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RU2009134982A (ru
Inventor
Валери ФРУСТИ
Бернар ДЮПРИЕ
Фабрис ГАНТИ
Original Assignee
Эрбюс Операсьон (Сас)
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
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Publication date
Application filed by Эрбюс Операсьон (Сас) filed Critical Эрбюс Операсьон (Сас)
Publication of RU2009134982A publication Critical patent/RU2009134982A/ru
Application granted granted Critical
Publication of RU2468226C2 publication Critical patent/RU2468226C2/ru

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
    • F02C7/047—Heating to prevent icing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0206—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0286—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turbofan engines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2250/00—Geometry
    • F05D2250/20—Three-dimensional
    • F05D2250/28—Three-dimensional patterned
    • F05D2250/283—Three-dimensional patterned honeycomb
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/96—Preventing, counteracting or reducing vibration or noise

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Exhaust Silencers (AREA)
  • Application Of Or Painting With Fluid Materials (AREA)
  • Surgical Instruments (AREA)
  • Wind Motors (AREA)
RU2009134982/06A 2007-02-20 2008-02-14 Покрытие для акустической обработки, передняя кромка и воздухозаборник летательного аппарата, содержащие такое покрытие RU2468226C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR0753358 2007-02-20
FR0753358A FR2912781B1 (fr) 2007-02-20 2007-02-20 Revetement pour le traitement acoustique integrant la fonction de traitement du givre avec de l'air chaud
PCT/FR2008/050244 WO2008104714A2 (fr) 2007-02-20 2008-02-14 Revetement pour le traitement acoustique integrant la fonction de traitement du givre avec de l'air chaud

Publications (2)

Publication Number Publication Date
RU2009134982A RU2009134982A (ru) 2011-03-27
RU2468226C2 true RU2468226C2 (ru) 2012-11-27

Family

ID=38477324

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2009134982/06A RU2468226C2 (ru) 2007-02-20 2008-02-14 Покрытие для акустической обработки, передняя кромка и воздухозаборник летательного аппарата, содержащие такое покрытие

Country Status (9)

Country Link
US (1) US7938224B2 (ja)
EP (1) EP2118471B1 (ja)
JP (1) JP5083918B2 (ja)
CN (1) CN101631941B (ja)
BR (1) BRPI0807277A2 (ja)
CA (1) CA2678368C (ja)
FR (1) FR2912781B1 (ja)
RU (1) RU2468226C2 (ja)
WO (1) WO2008104714A2 (ja)

Cited By (1)

* Cited by examiner, † Cited by third party
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RU2794016C2 (ru) * 2018-12-04 2023-04-11 Сафран Насель Воздухозаборник и способ борьбы с обледенением воздухозаборника гондолы авиационного турбореактивного двигателя

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EP2140120A2 (fr) * 2007-02-20 2010-01-06 AIRBUS France Procede de realisation d'un revetement pour le traitement acoustique incorporant une structure alveolaire avec une forme complexe et revetement pour le traitement acoustique ainsi obtenu
FR2950289B1 (fr) * 2009-09-23 2012-06-01 Airbus Operations Sas Procede de fabrication d'un reseau de conduits de drainage
EP2393711B1 (fr) * 2009-02-03 2015-08-19 Airbus Opérations SAS Panneau pour le traitement acoustique plus particulierement adapte a une entree d'air d'une nacelle d'aeronef
US8628635B2 (en) 2009-02-03 2014-01-14 Airbus Operations Sas Method for making a network of drainage pipes and acoustic processing panel including such a network of drainage pipes
FR2953811B1 (fr) * 2009-12-15 2012-03-16 Airbus Operations Sas Panneau pour une entree d'air d'une nacelle d'aeronef assurant un traitement acoustique et un traitement du givre optimises
JP2011183922A (ja) * 2010-03-08 2011-09-22 Mitsubishi Heavy Ind Ltd 航空機における翼前縁部の防除氷装置及び航空機主翼
FR2969702B1 (fr) * 2010-12-23 2014-10-10 Ge Energy Products France Snc Enceinte pour equipement thermique et procede de montage
FR2979385A1 (fr) * 2011-08-22 2013-03-01 Snecma Panneau d'isolation acoustique pour turbomachine et turbomachine comportant un tel panneau
FR2981049B1 (fr) * 2011-10-07 2014-04-11 Aircelle Sa Procede de fabrication d'un panneau d'absorption acoustique
FR2983835B1 (fr) * 2011-12-13 2014-02-21 Airbus Operations Sas Procede de realisation d'un panneau pour le traitement acoustique
CN102431650B (zh) * 2011-12-27 2015-08-19 东南大学 飞机翼型超声波辅助热气联合防除冰装置
US8919494B2 (en) 2012-07-31 2014-12-30 Rohr, Inc. Electric heater for integration into an aircraft acoustic panel
FR3013329B1 (fr) 2013-11-15 2017-08-11 Aircelle Sa Dispositif de degivrage d’entree d’air de nacelle d’un moteur d’aeronef, procede de fabrication d’un tel dispositif de degivrage et nacelle de moteur d’aeronef equipe d’un tel dispositif de degivrage
US9951690B2 (en) * 2014-08-19 2018-04-24 Pratt & Whitney Canada Corp. Low noise aeroengine inlet system
US10054050B2 (en) 2014-08-19 2018-08-21 Pratt & Whitney Canada Corp. Low noise aeroengine inlet system
US10221764B2 (en) 2014-08-19 2019-03-05 Pratt & Whitney Canada Corp. Variable geometry inlet system
US9957889B2 (en) 2014-08-19 2018-05-01 Pratt & Whitney Canada Corp. Low noise aeroengine inlet system
FR3041937B1 (fr) * 2015-10-05 2017-10-20 Airbus Operations Sas Structure compartimentee pour le traitement acoustique et le degivrage d'une nacelle d'aeronef et nacelle d'aeronef incorporant ladite structure
US10040535B2 (en) * 2015-12-02 2018-08-07 Embraer S.A. Composite accoustical panels especially useful for interior panel assemblies of aircraft passenger cabins
FR3051019B1 (fr) * 2016-05-03 2020-01-10 Airbus Operations Structure assurant une attenuation d'ondes acoustiques et un echange thermique
US10323532B2 (en) 2016-05-19 2019-06-18 General Electric Company Flow discourager and method of making same
US20180029719A1 (en) * 2016-07-28 2018-02-01 The Boeing Company Drag reducing liner assembly and methods of assembling the same
FR3065473B1 (fr) * 2017-04-25 2019-04-19 Airbus Operations Panneau pour le traitement acoustique comprenant des alveoles contenant chacune une pluralite de conduits
US20190062569A1 (en) * 2017-08-22 2019-02-28 Rohr, Inc. Laminar flow coating for aerodynamic surfaces
US10851713B2 (en) * 2017-08-29 2020-12-01 Mra Systems, Llc. Acoustic liner having internal structure
FR3070674B1 (fr) 2017-09-06 2019-09-13 Safran Nacelles Integration a la levre acoustique degivree
US11125157B2 (en) * 2017-09-22 2021-09-21 The Boeing Company Advanced inlet design
US10785831B2 (en) 2017-10-20 2020-09-22 Goodrich Corporation Micro-perforations for CNT heaters
US11052987B2 (en) * 2018-05-30 2021-07-06 The Boeing Company Integrally damped composite aircraft floor panels
FR3089252B1 (fr) 2018-12-04 2022-06-24 Safran Nacelles Dispositif et procédé de dégivrage d'une entrée d'air d’une nacelle d'un turboréacteur d'aéronef
GB2583751B (en) * 2019-05-09 2022-02-02 Safran Nacelles Ltd Acoustic panel
FR3100842A1 (fr) * 2019-09-12 2021-03-19 Airbus Operations Entrée d'air, nacelle, ensemble propulsif et aéronef à lèvre rainurée
GB2588204B (en) 2019-10-15 2022-09-14 Safran Nacelles Ltd Aircraft nacelle inlet
FR3103520B1 (fr) 2019-11-27 2022-07-29 Safran Nacelles Entrée d’air et procédé de dégivrage d'une entrée d'air d’une nacelle d'un turboréacteur d'aéronef

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US5743488A (en) * 1994-12-05 1998-04-28 Short Brothers Plc Aerodynamic low drag structure
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US20060219475A1 (en) * 2005-03-30 2006-10-05 Olsen Ronald F Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods

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Publication number Priority date Publication date Assignee Title
US3933327A (en) * 1974-08-30 1976-01-20 Rohr Industries, Inc. Aircraft anti-icing plenum
US5743488A (en) * 1994-12-05 1998-04-28 Short Brothers Plc Aerodynamic low drag structure
US5841079A (en) * 1997-11-03 1998-11-24 Northrop Grumman Corporation Combined acoustic and anti-ice engine inlet liner
US6698691B2 (en) * 2001-02-15 2004-03-02 Airbus France Process for de-icing by forced circulation of a fluid, an air intake cowling of a reaction motor and device for practicing the same
RU2280186C2 (ru) * 2004-07-22 2006-07-20 Открытое акционерное общество "Авиадвигатель" Устройство для звукопоглощения в двухконтурном турбореактивном двигателе
US20060219475A1 (en) * 2005-03-30 2006-10-05 Olsen Ronald F Flow restrictors for aircraft inlet acoustic treatments, and associated systems and methods

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2794016C2 (ru) * 2018-12-04 2023-04-11 Сафран Насель Воздухозаборник и способ борьбы с обледенением воздухозаборника гондолы авиационного турбореактивного двигателя

Also Published As

Publication number Publication date
JP5083918B2 (ja) 2012-11-28
JP2010519098A (ja) 2010-06-03
WO2008104714A2 (fr) 2008-09-04
WO2008104714A3 (fr) 2008-11-13
RU2009134982A (ru) 2011-03-27
BRPI0807277A2 (pt) 2014-05-06
US20100096213A1 (en) 2010-04-22
FR2912781A1 (fr) 2008-08-22
CN101631941A (zh) 2010-01-20
CA2678368C (fr) 2015-09-29
EP2118471B1 (fr) 2012-06-27
CN101631941B (zh) 2013-06-12
FR2912781B1 (fr) 2009-04-10
EP2118471A2 (fr) 2009-11-18
CA2678368A1 (fr) 2008-09-04
US7938224B2 (en) 2011-05-10

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20210215